TASK 72-00-40-420-006-A00 HP System Module - Install And Connect The Components, Electrical Harnesses, And Tubes On The Front Of The HPC Case, Installation-009

DMC:V2500-A1-72-00-4000-06B-720A-B|Issue No:002.00|Issue Date:2013-11-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

V2500-A1

Common Information

TASK 72-00-40-420-006-A00 HP System Module - Install And Connect The Components, Electrical Harnesses, And Tubes On The Front Of The HPC Case, Installation-009

General

This TASK gives the procedure to install and connect the components, the electrical harnesses and the tubes at the front of the HP system module. Refer to the TASKs which follow for other related procedures.

TASK 72-00-40-420-004 (INSTALLATION-007) Install the Initial components and the air Off-take ducts.

TASK 72-00-40-420-005 (INSTALLATION-008) Install the components, the ducts, the electrical harnesses and the tubes to the HP compressor vertical splitline.

TASK 72-00-40-420-007-A00 (INSTALLATION-10, CONFIG-01) Install the components, the electrical harnesses, the tubes and the brackets to the HP turbine.

Fig./item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig./item numbers are used. For the service bulletin alpha variants refer to the IPC.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig./item number.

Assembly tolerances are included in this procedure.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS approved engine oil unless other lubricants are referred to in the procedure.

Special torque data is identified with the symbol * after the torque value.

For the torque tightening procedures refer to the SPM TASK 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-410-501.

To identify, lubricate and install seal rings refer to the SPM TASK 70-44-01-400-501.

For lockwire data and procedures refer to the SPM TASK 70-42-05-400-501.

For safety cable data and procedures refer to the SPM TASK 70-42-08-400-501.

Safety the threaded fasteners in this TASK with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT for the ATA Chapter/Section/Subjects which follow:

A1 series engines:

71-51-41

71-52-43

72-41-34

73-22-49

75-23-49

75-31-42

75-31-43

75-32-42

75-00-49

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attachment parts. Use the correct color of air drying enamel. Refer to the SPM TASK 70-38-21-380-501.

The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.

Transportation covers/blanks must not be removed until immediately before installation of the components.

Do not remove the special plastic caps from electrical connections until immediately before installation. This will give protection from unwanted material.

NOTE

To identify the consumable materials refer to the PCI.
SBE 70-0813 : Announcement of introduction of safety cable as a preferred method to lockwire.
Safety the threaded fasteners in this TASK with safety cable for the ATA Chapter/Section/Subjects detailed in 2. General.

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
0.937 in. (24.00 mm) crowsfoot spannerLOCAL0.937 in. (24.00 mm) crowsfoot spanner
IAE 1N20014 Forward engine mount sling0AM53IAE 1N200141
IAE 1R18000 Wrench0AM53IAE 1R180001
IAE 1R18001 Wrench0AM53IAE 1R180011
IAE 1R18003 Wrench0AM53IAE 1R180031
IAE 1R18254 Rigging pin0AM53IAE 1R182541
IAE 1R18282 Rigging pin0AM53IAE 1R182821

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-001 SOLVENT, DELETED0AM53CoMat 01-001
CoMat 02-099 LINT-FREE CLOTHLOCALCoMat 02-099
CoMat 02-119 LOCKWIRELOCALCoMat 02-119
CoMat 02-126 LOCKWIRELOCALCoMat 02-126
CoMat 02-141 LOCKWIRELOCALCoMat 02-141
CoMat 02-146 LOCKWIRELOCALCoMat 02-146
CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)LOCALCoMat 02-148
CoMat 02-159 LACING TAPELOCALCoMat 02-159
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADELOCALCoMat 04-005
CoMat 05-016 GARNET PAPER, 80-GRITLOCALCoMat 05-016
CoMat 05-017 GARNET PAPER, 60 GRITLOCALCoMat 05-017
CoMat 07-038 AIR DRYING ENAMELK3504CoMat 07-038
CoMat 08-013 COLD CURING SILICONE COMPOUNDLOCALCoMat 08-013
CoMat 08-074 SEALANT, RTV SILICONE01139CoMat 08-074
CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT0AM53CoMat 08-014
CoMat 08-032 PRIMERLOCALCoMat 08-032
CoMat 10-038 PETROLEUM JELLYLOCALCoMat 10-038
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 10-060 LIQUID PARAFFINLOCALCoMat 10-060
CoMat 01-002 SOLVENT, DELETED.0AM53CoMat 01-002

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Seal ring1
Sealing ring1
Preformed packing1
Packing2
Packing2
Packing2
Packing2
Packing2
Packing2
Packing2
Packing2
Preformed packing1
Keywasher1
Keywasher1
Packing1

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-40-420-099 Connect the Tubes at the Bifurcation Panel

    1. Refer to Figure, Figure and Figure.

      2. NOTE

        The connectors of the tubes 60 and 61 are tightened and safetied in Step.

        Connect the fuel tubes at the bifurcation panel.

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-096) preformed packing1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY.

      2. Install the preformed packing on the tube 93 and loosely connect the tube 60.

      3. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 19-498) preformed packing1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY.

      4. Install the preformed packing on the tube 106 and loosely connect the tube 61.

      3. CAUTION

        YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

        Connect the oil tubes at the bifurcation panel.

      1. Connect the tube 20 to the tube 124. With IAE 1R18001 Wrench 1 off torque the tube connector to 398 to 434 lbf.in (45 to 49 Nm) and safety with CoMat 02-126 LOCKWIRE.

        2. Connect the tube 55:

        1. Connect the tube 55 to the tube 127. Tighten the nut by hand.

        2. Torque the tube nut at the diffuser case to 478 to 513 lbf.in (54 to 58 Nm).

        3. With IAE 1R18003 Wrench 1 off torque the tube connector at the bifurcation panel to 566 to 611 lbf.in (64 to 69 Nm).

          4. Check the tube 55 at the diffuser case:

          1. Fully loosen the tube nut at the diffuser case.

          2. Make sure that the tube is still aligned and in free condition.

          3. If the tube is still aligned and in free condition, torque the nut to 566 to 611 lbf.in (64 to 69 Nm).

          4. If the tube has moved repeat Step to Step.

        5. Safety the tube nut and tube connector with CoMat 02-126 LOCKWIRE.

      4. CAUTION

        YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

        Connect the air tubes at the bifurcation panel.

      1. Connect the tube 16 to the tube 168 and torque the tube connector to 283 to 310 lbf.in (32 to 35 Nm). Safety with CoMat 02-126 LOCKWIRE.

      2. Connect the tube 56 to the tube 157 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      3. Connect the tube 69 to the tube 143 and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

      4. Connect the tube 68 to the tube 162 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      5. Connect the tube 53 to the tube 138 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      6. Connect the tube 32 to the tube 161 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      7. Connect the tube 63 to the tube 156 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      8. Connect the tube 48 to the tube 153 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      9. Connect the tube 64 to the tube 166 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

      10. Connect the tube 65 to the tube 145 and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE.

    2. SUBTASK 72-00-40-420-077 Install the Active Clearance Control (ACC) Actuator

    1. Refer to Figure and Figure

    2. Attach the ACC actuator to the bracket ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-118) with the two bolts AIR-ACTIVE CLEARANCE CONTROL ACTUATOR (75-24-52, 01-174) and the nuts AIR-ACTIVE CLEARANCE CONTROL ACTUATOR (75-24-52, 01-171). Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    3. Install the two bolts AIR-ACTIVE CLEARANCE CONTROL ACTUATOR (75-24-52, 01-120) that attach the ACC actuator to the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-380). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

    3. SUBTASK 72-00-40-420-078 Install the Variable Stator Vane (VSV) Actuator,.nd (Pre SBE 70-0158, Pre SBE 75-0034, SBE 70-0158, SBE 75-0034, Pre SBE 75-0055 and SBE 72-0398)

      NOTE

      SBE 72-0398 has removed the requirement for SBE 75-0055.

      SBE 70-0158: Information - Introduce various revised material external brackets

      SBE 75-0034: Air - Replace HPC VSV actuator bracket assembly

      SBE 72-0398: Re-Introduction of a standard variable stator vane schedule

    1. Refer to Figure and Figure

    2. WARNING

      WHEN YOU USE CoMat 01-001 SOLVENT, DELETED INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.

      With CoMat 01-001 SOLVENT, DELETED; clean the bolts AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-082 , 01-102 and 01-112), the brackets AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070 and 01-080) and the attachment faces of the VSV actuator and the HP compressor case. Then apply a layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE to the surfaces and the bolts.

    3. Attach the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-080) to the VSV actuator with the bolt AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-112) and tighten by hand.

    4. Attach the VSV actuator to the HP compressor case with the four bolts AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-102 and 01-082), the two washers AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-104) and the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070). Tighten by hand.

    5. Torque the two bolts AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-102) to 180 to 220 lbf.in (20 to 25 Nm).

    6. Torque the two bolts (75-32-41, 01-082) to 180 to 220 lbf.in (20 to 25 Nm).

    7. Torque the two bolts AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-112) to 180 to 220 lbf.in (20 to 25 Nm).

      8. Pre SBE 75-0055 and SBE 72-0398 : Connect the VSV actuator to the actuating mechanism.

      1. Move the VSV actuating mechanism to the high speed position.

      2. Install IAE 1R18254 Rigging pin 1 off through the bearing housing and locate in the crankshaft recess.

      3. Install IAE 1R18282 Rigging pin 1 off in the actuating ram.

      4. Loosely assemble the control rod and adjust the length such that the bolt HP COMP VARIABLE STATOR VANE ACTUATOR LINKAGE (75-32-42, 01-084) and the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 07-081) can be installed. Make sure that the control rod ends are in safety with an applicable probe, and lock them with the locknuts. Make sure control rod end alignment is correct.

      5. Install the washer HP COMP VARIABLE STATOR VANE ACTUATOR LINKAGE (75-32-42, 01-083), the washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 07-080), the nut HP COMP VARIABLE STATOR VANE ACTUATOR LINKAGE (75-32-42, 01-082) and the nut ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 07-082) to attach the control rod to the actuator and the ram actuating lever on the crankshaft.

      6. Align the D-head of each of the bolts with the stepped section of the actuator fork and crankshaft lever. Torque the nuts to 290 to 370 lbf.in (33 to 42 Nm).

      7. Safety the control rod locknuts with CoMat 02-119 LOCKWIRE.

      8. Remove the two rigging pins.

    4. SUBTASK 72-00-40-420-101-A00 Install the Raceways (Pre SBE 72-0132, Pre SBE 75-0016 and SBE 70-0034)

    1. Refer to Figure.

    2. SBE 70-0034: catalog sequence number change at CP5644

      3. Install the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-500). Figure.

        1. Assemble the clip position 5699.

        1. Attach the raceway to the ignition exciter air inlet fitting bracket AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-450) on the inside of the LP compressor/intermediate case with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-502), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-504) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-506). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        2. Assemble the clip position 5644.

        1. Pre SBE 70-0034 : Install the clip V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-528) on the raceway adjacent to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-548) on the LP compressor/intermediate case rear frame.

        2. Attach the clip to the bracket with the bolt V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-525), the washer V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-526) and the clipnut V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-532). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        3. SBE 70-0034 : Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-528) on the raceway adjacent to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-548) on the LP compressor/intermediate case rear frame.

        4. Attach the clip to the bracket with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-525), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-526) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-532). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      4. Install the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-100). Figure.

        1. Assemble the clip position 5676.

        1. Attach the raceway to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-535) on the LP compressor/intermediate case rear frame with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-102), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-104) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-106). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      2. Assemble the clip positions 5640, 5650, 5802 and 5803 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Figure.nd Figure.

    5. SUBTASK 72-00-40-420-101-B00 Install the Raceways (SBE 72-0132, SBE 75-0016 and SBE 70-0034)

      SBE 72-0132: LP compressor - Removal of stage 6 buffer air system

      SBE 75-0016: Air - HPC bleed air tubes - Revised core engine tubes to improve clearance with harness in bifurcation area - RH side

      SBE 70-0034: catalog sequence number change at CP5644

    1. Refer to Figure.

      2. Install the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-500). Refer to Figure.

        1. Assemble the clip position 5699.

        1. Attach the raceway to the ignition exciter air inlet fitting bracket AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-450) on the inside of the LP compressor/intermediate case with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-502), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-504) and the clipnuts BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-506). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        2. Assemble the clip position 5644.

        1. Pre SBE 70-0034 : Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-128) on the raceway adjacent to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-548) on the LP compressor/intermediate case rear frame.

        2. Attach the clip to the bracket with the bolt V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-525), the washer V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-526) and the clipnut V2500-A5-71-52-50-01A-941A-D (71-52-50, 01-532). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        3. SBE 70-0034 : Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-528) on the raceway adjacent to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-548) on the LP compressor/intermediate case rear frame.

        4. Attach the clip to the bracket with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-525), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-526) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-532). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      3. Install the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-100). Refer to Figure.

        1. Assemble the clip position 5676.

        1. Attach the raceway to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE(72-32-00, 02-535) on the LP compressor/intermediate case rear frame with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-102), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-104) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-106). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      2. Assemble the clip positions 5650, 5802 and 5803 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      4. Install the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-100). Refer to Figure.

        1. Assemble clip position 5427.

        1. Attach the raceway to the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-530) on flange J, with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-125), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-126) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-132). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        2. Assemble clip position 6057.

        1. Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-144) on the raceway adjacent to the bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-180) on the LP compressor bleed valve actuator bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-200).

        2. Attach the clip to the bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-180) with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-141), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-142) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-148). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        3. Assemble clip position 5746. Refer to Figure.

        1. Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-136) on the raceway adjacent to the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070).

        2. Attach the clip to the bracket with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-133) the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-134) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-140). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    6. SUBTASK 72-00-40-420-126 Install the HP Servo Fuel Tubes 60 and 61

    1. Refer to Figure, Figure and Figure

    2. NOTE

      The tubes 60 and 61 are attached to the bifurcation panel in Step, but the connectors were not fully tightened.

      3. Assemble clip position 5668, Refer to Figure.

      1. Put the clips ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-152 and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE 19-536) on the tubes 60 and 61 adjacent to the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-510) on the HP compressor/diffuser case splitline.

      2. Attach the clips to the bracket with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-149), the washer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-150), the two spacers ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-154) and the clipnut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 11-156). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    4. CAUTION

      YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

      Torque the tube connectors at the bifurcation panel to 660 to 735 lbf.in (74,6 to 83 Nm) and safety with CoMat 02-126 LOCKWIRE.

    5. Assemble the clip positions 5667, 5666 and 5653 and torque the nuts and the bolt to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.nd Figure.

    7. SUBTASK 72-00-40-420-204 Install the HP Servo Fuel Tubes 27, 28 and 44

    1. Refer to Figure and Figure.

      2. Install the tubes 27, 28 and 44 (ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 18-100), ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 13-100) and ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-500)).

      1. Lightly lubricate two new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 18-096) packing 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install one packing on the lower connection of the tube 61 and one packing on the ACC actuator connection. Refer to Figure and Figure.

      2. Lightly lubricate two new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 13-096) packing 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install one packing on the front connection of the tube 60 and one packing on the ACC actuator connection. Refer to Figure and Figure.

      3. Lightly lubricate two new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-496) packing 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install one packing on the lower connection of the tube 60 and one packing on the VSV actuator connection. Refer to Figure and Figure.

      4. Connect the tube 27 to the tube 61 and to the ACC actuator. Torque the tube connectors to 330 to 360 lbf.in (37.3 to 40.7 Nm) and safety with CoMat 02-126 LOCKWIRE. Refer to Figure and Figure.

      5. Connect the tube 28 to the tube 60 and the ACC actuator. Torque the tube connectors to 425 to 475 lbf.in (48 to 53.7 Nm) and safety with CoMat 02-126 LOCKWIRE. Refer to Figure.nd Figure.

      6. Connect the tube 44 to the tube 60 and to the VSV actuator. Torque the tube connectors to 425 to 475 lbf.in (48 to 53.7 Nm) and safety with CoMat 02-126 LOCKWIRE. Use a 0.937 in. (24 mm) crowsfoot spanner to torque the VSV tube connector. Refer to Figure and Figure.

    3. Assemble the clip positions 5670 and 5748 and torque the nuts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure and Figure.

    8. SUBTASK 72-00-40-420-205 Install the HP Servo Fuel Tube 41

    1. Refer to Figure and Figure.

      2. NOTE

        The other end of the tube 41 will be connected to the LP compressor master actuator in SUBTASK 72-00-04-420-107.

        Install the tube 41 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-100).

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the upper connection of the tube 61. Refer to Figure.

      2. Put the tube 41 in position and connect it to the tube 61. Refer to Figure.

    3. Loosely assemble the clip positions 5648 and 5783. Refer to Figure and Figure.

    4. Torque the tube connector to 330 to 360 lbf.in (37.3 to 40.7 Nm) and safety with CoMat 02-126 LOCKWIRE. Torque the clip position nuts to 36 to 45 lbf.in (4 to 5 Nm).

    9. SUBTASK 72-00-40-420-206-A00 Install the HP Servo Fuel Tube 43 (Pre SBE 72-0027, Pre SBE 72-0132 and Pre SBE 73-0103)

    1. Refer to Figure and Figure.

      2. NOTE

        The other end of the tube 43 will be connected to the LP compressor master actuator in SUBTASK 72-00-04-420-107.

        Install the tube 43 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-100).

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-096) packing1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the upper connection of the tube 60. Refer to Figure.

      2. Put the tube 43 in position and connect it to the tube 60. Refer to Figure.

    3. Loosely assemble the clip position 5701. Refer to Figure.

    4. Torque the tube connector to 425 to 475 lbf.in (48 to 53,7 Nm) and safety with CoMat 02-126 LOCKWIRE. Torque the clip position bolt to 36 to 45 lbf.in (4 to 5 Nm).

    10. SUBTASK 72-00-40-420-206-B00 Install the HP Servo Fuel Tube 43 (SBE 72-0132)

      SBE 72-0132: LP Compressor - Removal of stage 6 buffer air system

    1. Refer to Figure.

      2. NOTE

        The other end of the tube 43 will be connected to the LP compressor master actuator in SUBTASK 72-00-04-420-107.

        Install the tube 43 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-100).

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the upper connection of tube 60. Refer to Figure.

      2. Put the tube 43 in position and connect it to the tube 60. Refer to Figure.

    3. Loosely assemble the clip position 5701. Refer to Figure.

    4. Torque the tube connector to 425 to 475 lbf.in (48 to 53.7 Nm) and safety with CoMat 02-126 LOCKWIRE. Torque the clip position bolt to 36 to 45 lbfin (4 to 5 Nm).

      5. Assemble the clip position 5747. Refer to Figure.

      1. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-168) on tube 43 above clip position 5701.

      2. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-168) on tube 41 above clip position 5701.

      3. Connect the two clips together with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-165), the two washers ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-166) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-172). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

      6. Assemble the clip position 6058. Refer to Figure and Figure.

      1. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-176) on tube 43 adjacent to the lug on the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-100).

      2. Attach the clip to the lug on the raceway with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-173) the two washers ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-174), the spacer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-178) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-180). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    11. SUBTASK 72-00-40-420-206-C00 Install the HP Servo Fuel Tube 43 (SBE 72-0027, SBE 73-0115 and SBE 73-0103)

      SBE 72-0027: HP Compressor - Introduction of reduced weight front compressor casing

      SBE 73-0115: Engine fuel and control - Fuel system tubes - Engine - Introduction of revised external fuel tube assembly with welded-in lug and amended clipping

      SBE 73-0103: Engine fuel and control - Fuel system tubes - Engine - Introduction of revised clipping for the HP servo external fuel tube assembly

    1. Refer to Figure.

      2. NOTE

        The other end of the tube 43 will be connected to the LP compressor master actuator in SUBTASK 72-00-04-420-107.

        Install the tube 43 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-100).

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the upper connection of tube 60. Refer to Figure.

      2. Put the tube 43 in position and connect it to the tube 60. Refer to Figure.

    3. Loosely assemble the clip position 5701. Refer to Figure and Figure.

    4. Torque the tube connector to 425 to 475 lbf.in (48 to 53.7) and safety with CoMat 02-126 LOCKWIRE. Torque the clip position bolt to 36 to 45 lbf.in (4 to 5 Nm).

      5. Pre SBE 73-0115: Assemble the clip position 5747. Refer to Figure.

      1. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-168) on tube 43 above clip position 5701.

      2. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-168) on tube 41 above clip position 5701.

      3. Connect the two clips together with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-165), the two washers ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-166), the spacer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-170) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-172). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

      6. SBE 73-0115: Assemble the clip position 5747. Refer to Figure.

      1. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-168) on tube 43 above clip position 5701.

      2. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-168) on tube 41 above clip position 5701.

      3. Connect the two clips together with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-165), the washer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-166), the spacer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-170) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-172). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

      7. Assemble the clip position 6058. Refer to Figure and Figure.

      1. Install the clip ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-176) on tube 43 adjacent to the lug on the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-100).

      2. Pre SBE 73-0103: Attach the clip to the lug on the raceway with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-173), the two washers ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-174), the spacer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-178) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-180). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

      3. SBE 73-0103: Attach the clip to the lug on the raceway with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-173), the washer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-174), the spacer ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-178) and the nut ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-180). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    12. SUBTASK 72-00-40-420-207 Install the HP Servo Fuel Tubes 33 and 34

    1. Refer to Figure and Figure

      1. Put the tubes 33 and 34 in position on the HP compressor case.

      2. NOTE

        These clip positions are tightened in Step.

        Loosely assemble the clip positions 5672, 5673, 5778, 5769 and 5775. Refer to Figure and Figure.

    13. SUBTASK 72-00-40-420-130 Install the Fuel Distribution Feed Tube 62

    1. Refer to Figure, Figure, Figure and Figure

      2. Install the tube 62 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 09-100).

      1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 08-090) seal ring1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the seal ring on the tube 95 at the bifurcation panel.

      2. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 09-116) sealing ring1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the sealing ring on the tube 62.

      3. Attach the tube 62 to the fuel distribution valve with the three bolts ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 09-114) and torque them to 85 to 105 lbf.in (10 to 12 Nm).

      4. CAUTION

        YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

        Connect the tube 62 to the tube 95 and torque the tube connector to 1150 to 1250 lbf.in (130 to 141 Nm). Safety with CoMat 02-126 LOCKWIRE.

    14. SUBTASK 72-00-40-420-127 Install the HP Fuel Servo Tube 46 and the P2.5 Air Tubes 66 and 67

      1. Install the tube 66 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 09-100). Refer to Figure and Figure.

      1. Connect the tube 66 to the air tube ENGINE-INTERMEDIATE STRUCTURE (72-32-03, 01-550) at the LP compressor/intermediate case rear frame. Refer to Figure.

      2. Assemble the clip position 5777 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      2. Install the tube 67 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 09-500). Refer to Figure.

      1. Connect the tube 67 to the tube 66 and to the tube 243 ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 10-100) at the bifurcation panel. Refer to Figure and Figure.

      2. Assemble the clip positions 5700 and 5704 and torque the nuts to 36 to 45 lbfin (4 to 5 Nm). Refer to Figure.

      3. CAUTION

        YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

        Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      3. Install the tube 46 ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 19-100). Refer to Figure.

      1. Lightly lubricate two new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 19-096) packing 2 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install one packing on the front connection of the tube 61 and one packing on the VSV actuator connection. Refer to Figure and Figure.

      2. Connect the tube 46 to the tube 61 and to the VSV actuator.

      3. Assemble the clip positions 5770 and 5766 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure and Figure.

      4. Torque the tube connectors to 425 to 475 lbf.in (48 to 53.7 Nm) and safety with CoMat 02-126 LOCKWIRE.

    15. SUBTASK 72-00-40-420-102 Install the No. 1, 2 and 3 Bearing Oil Feed Tubes 57 and 58

    1. Refer to Figure, Figure, Figure and Figure.

    2. Lightly lubricate a new OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 11-116) packing 1 off with CoMat 10-077 APPROVED ENGINE OILS and install it on the tube 58.

    3. Install the three bolts OIL-PRESSURE OIL TUBES-ENGINE (79-21-49, 11-114) that attach the tube 58 to the oil feed adapter and torque to 85 to 105 lbf.in (10 to 12 Nm).

    4. Connect the tube 57 to the tube 177 at the bifurcation panel and to the tubes 23, 24 and 58.

    5. Assemble the clip position 5658 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    6. Torque the tube connector of the tube 24 to 257 to 283 lbf.in (29 to 32 Nm) and safety with CoMat 02-126 LOCKWIRE.

    7. Torque the tube connector of the tube 23 to 204 to 221 lbf.in (23 to 25 Nm) and safety with CoMat 02-126 LOCKWIRE.

    8. CAUTION

      YOU MUST STOP THE TUBE TURNING WHEN YOU TORQUE THE TUBE NUTS. USE A SPANNER ON THE REAR OF THE MATING UNION. THIS WILL PREVENT ANY STRAIN ON THE TUBES AND HELP PREVENT LEAKS.

      With IAE 1R18001 Wrench 1 off torque the tube connector of the tube 57 to 398 to 434 lbf.in (45 to 49 Nm). Safety with CoMat 02-126 LOCKWIRE.

    9. With IAE 1R18000 Wrench 1 off torque the tube connector of the tube 58 to 319 to 345 lbf.in (36 to 39 Nm). Safety with CoMat 02-126 LOCKWIRE.

    16. SUBTASK 72-00-40-420-103-A00 Install the Front Bearing Buffer Air Tubes 30 and 39 (Pre SBE 75-0011 and Pre SBE 72-0132)

    1. Refer to Figure, Figure, Figure and Figure.

      2. Install the tube 30 AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-100).

      1. Install the C seal AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-078) and attach the tube 30 to the LP compressor/intermediate case rear frame with the three bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-114). Attach the tube 30 to the HP compressor case with the two bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-106). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

      3. Install the tube 39 AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-100).

      1. Install the C seal AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-078) and attach the tube 39 to the LP compressor/intermediate case rear frame with the three bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-114). Attach the tube 39 to the HP compressor case with the two bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-106). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

    4. Assemble the clip positions 5776, 5749, 5747 and 5746 and torque the nuts and bolts to 36 to 45 lbf.in (4 to 5 Nm).

    17. SUBTASK 72-00-40-420-103-B00 Install the Front Bearing Buffer Air Tubes 30 and 39 (Pre SBE 72-0132 and SBE 75-0011)

      SBE 75-0011: Air - Introduction of a support bracket for the FBC buffer air tube assembly

    1. Refer to Figure, Figure, Figure and Figure.

      2. Install the tube 30 AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-100).

      1. Install the C seal AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-078) and attach the tube 30 to the LP compressor/intermediate case rear frame with the three bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-114). Attach the tube 30 to the HP compressor case with the two bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 11-106). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

      3. Install the tube 39 AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-100).

      1. Install the C seal AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-078) and attach the tube 39 to the LP compressor/intermediate case rear frame with the three bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-114). Attach the tube 39 to the HP compressor case with the two bolts AIR-BEARING COMPARTMENT COOLING & SEALING TUBES (75-22-49, 13-106). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

    4. Assemble the clip positions 5776, 5749, 5799, 5747 and 5746 and torque the nuts and bolts to 36 to 45 lbf.in (4 to 5 Nm).

    18. SUBTASK 72-00-40-420-131 Electrical Harness Installation Procedure (SBE 71-0109)

      SBE 71-0109: Provide improved routing and clipping of the EEC and Ignition supply harness and raceway

    1. Refer to Figure.

    2. During the installation procedure make sure the harnesses are held temporarily along their different lengths. Always install the datum clip positions when you install each electrical connector. This will give correct installation of the different harnesses, prevent too much strain on the electrical connectors and give the necessary drip loops (the drip loop makes sure moisture or fluids do not go in to the electrical connector).

    3. Because of the differences between the harness diameters, the specified clip could be too large or too small. You can use a clip from a range of six clips that have the same part number. If the harness diameter is between two of the clips in the range, use the larger clip. When you do this use CoMat 02-148 ADHESIVE TAPE (ELECTRICAL) to increase the harness diameter.

    4. For the data on the electrical connectors refer to the SPM TASK 70-43-00-400-501 and the SPM 70-43-01-400-501.

    5. For the data on the installation of the open wire harness refer to the SPM TASK 70-43-02-400-501.

    6. SBE 71-0109 : Route and attach the right hand side and left hand side EEC harness looms together at the bifurcation panel electrical connectors 4008VC-A and 4009VC-A. Refer to Step.

    19. SUBTASK 72-00-40-420-104-A00 Install the Core Overheat Detector, the Ignition Supply Harness, the Fire Detection (System B) Harness and the EEC Harness

      1. The procedures that were in this SUBTASK have been transferred to the SUBTASKS that follow:

      1. Install the Core Overheat Detector, Step.

      2. Install the EEC Harness and the Fire Detection Harness, Step.

      3. Connect the EEC Harness to the Fan Speed Terminal Block, SUBTASK 72-00-40-420-213.

      4. Connect the EEC Harness to the T2.5 Thermocouple Terminal Block, Step.

      5. Install the Harness Clips and the Raceway ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-100), SUBTASK 72-00-40-420-215.

      6. Connect Electrical Connectors to the VSV, SUBTASK 72-00-40-420-216.

      7. Install the Ignition Supply Harness, Step.

    20. SUBTASK 72-00-40-420-104-B00 Install the Core Overheat Detector, the Ignition Supply Harness, the Fire Detection (System B) Harness and the EEC Harness

      1. The procedures that were in this SUBTASK have been transferred to the SUBTASKS that follow:

      1. Install the Core Overheat Detector, Step.

      2. Install the Raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE(71-52-50, 04-500), SUBTASK 70-11-40-420-210.

      3. Install the EEC Harness and the Fire Detection Harness, Step.

      4. Connect the EEC Harness to the Fan Speed Terminal Block, SUBTASK 72-00-40-420-213.

      5. Connect the EEC Harness to the T2.5 Thermocouple Terminal Block, Step.

      6. Install the Harness Clips and the Raceway ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-100), SUBTASK 72-00-40-420-215.

      7. Connect Electrical Connectors to the VSV, SUBTASK 72-00-40-420-216.

      8. Install the Ignition Supply Harness, Step.

    21. SUBTASK 72-00-40-420-211-A00 Install the Core Overheat Detector (26-12-19,01-100) (Pre SBN 70-0151)

    1. Refer to Figure, Figure, Figure and Figure.

    2. Attach the bracket FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 05-010) to the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-100) with the two bolts FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 05-015), the two washers FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 05-020) and the two nuts FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 05-025) at the clip positions 5802 and 5803. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    3. Attach the core overheat detector to the bracket with the four bolts FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 01-105), the four washers FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 01-107) and the four nuts FIRE PROTECTION-CORE ZONE OVERHEAT DETECTOR (26-12-19, 01-110). Torque the nuts to 6 to 8 lbf.in (0.68 to 0.90 Nm).

    4. Assemble the clip positions 5221 and 5223 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    5. Connect the electrical connector 4008KS-A and torque to 14 * lbf.in (1.6 Nm).

    22. SUBTASK 72-00-40-420-211-B00 Install the Core Overheat Detector (75-41-15,01-100) (SBN 70-0151)

      SBN 70-0151: ATA Chapter relocation of the nacelle temperature sensor

    1. Refer to Figure, Figure, Figure and Figure.

    2. Attach the bracket NACELLE TEMPERATURE SENSOR (75-41-15, 05-010) to the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 05-100) with the two bolts NACELLE TEMPERATURE SENSOR (75-41-15, 05-015), the two washers NACELLE TEMPERATURE SENSOR (75-41-15, 05-020) and the two nuts NACELLE TEMPERATURE SENSOR (75-41-15, 05-025) at the clip positions 5802 and 5803. Torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    3. Attach the core overheat detector to the bracket with the four bolts NACELLE TEMPERATURE SENSOR (75-41-15, 01-105), the four washers NACELLE TEMPERATURE SENSOR (75-41-15, 01-107) and the four nuts NACELLE TEMPERATURE SENSOR (75-41-15, 01-110). Torque the nuts to 6 to 8 lbf.in (0.68 to 0.90 Nm).

    4. Assemble the clip positions 5221 and 5223 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    5. Connect the electrical connector 4008KS-A and torque to 14 * lbf.in (1.6 Nm).

    23. SUBTASK 72-00-40-420-210 Install the Raceway (71-52-50,04-500) (SBE 72-0132)

      SBE 72-0132: LP compressor - Removal of stage 6 buffer air system

    1. Refer to Figure and Figure.

    2. Put the raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-500) in position.

      3. Assemble the clip position 5776.

      1. Attach the raceway to the bracket IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-270) with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-525), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-526) and the nut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-532). Lightly tighten the nut.

      4. Assemble the clip position 6056.

      1. Install the clip BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-535) on the raceway, adjacent to the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-260) on flange J.

      2. Attach the clip to the bracket with the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-533), the washer BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-534) and the clipnut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-540). Lightly tighten the bolt.

    5. Torque the nut BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-532) and the bolt BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-540) to 36 to 45 lbf.in (4 to 5 Nm).

    24. SUBTASK 72-00-40-420-212-A00 Install the EEC Harness and the Fire Detection (System B) Harness (Pre SBN 71-0145, SBN 71-0145, Pre SBE 71-0303, Pre SBE 72-0132, Pre SBE 79-0087 and SBE 79-0087)

      SBN 71-0145: Nacelle - Powerplant - Core fire detector - rework

      SBE 79-0087: Oil - Scavenge oil tubes - Reroute of number 4 bearing scavenge tube

    2. Install the EEC harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005) and the fire detection (System B) harness ELECT HARNESS-LIGHT DUTY-FIRE DETECTION SYSTEM B (71-52-42, 01-005).

    3. Attach the two electrical receptacles 4008VC and 4009VC (with the master keyways to the front) to the bifurcation panel with the eight bolts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-022) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-027) and the nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-020) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-025). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm). Connect the two electrical connectors 4008VC-A and 4009VC-A and torque to 55 * lbfin (6.2 Nm).

    4. Connect the electrical connector 4006VC-A to the EEC link harness receptacle and torque to 21 * lbf.in (2.4 Nm).

    5. Assemble the datum clip position 5750 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    6. Connect the electrical connector 4027KS-A to the ACC actuator and torque to 32 * lbf.in (3.6 Nm).

    7. Assemble the datum clip position 5711 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    8. Assemble the datum clip position 5765 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    9. Assemble the datum clip position 5693 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    10. Pre SBE 71-0145: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820, 5801 and 5800.

      SBE 71-0145 and Pre SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821 and 5820.

      SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 6126 and 6120.

      Torque the nuts and the bolts to 36 to 45 lbf.in (4 to 5 Nm).

    25. SUBTASK 72-00-40-420-212-B00 Install the EEC Harness and the Fire Detection (System B) Harness (Pre SBE 71-0109, Pre SBN 71-0145, SBN 71-0145, Pre SBE 71-0303, SBE 72-0132, SBE 75-0034, Pre SBE 79-0087 and SBE 79-0087)

      SBN 71-0145: Nacelle - Powerplant - Core fire detector - rework

      SBE 72-0132: LP compressor - Removal of stage 6 buffer air system

      SBE 75-0034: Air - Replace HPC VSV actuator bracket assembly

      SBE 79-0087: Oil - Scavenge oil tubes - Reroute of number 4 bearing scavenge tube

    2. Install the EEC harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005) and the fire detection (System B) harness ELECT HARNESS-LIGHT DUTY-FIRE DETECTION SYSTEM B (71-52-42, 01-005).

    3. Attach the two electrical receptacles 4008VC and 4009VC (with the master keyways to the front) to the bifurcation panel with the eight bolts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-022) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-027) and the nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-020) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-025). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm). Connect the two electrical connectors 4008VC-A and 4009VC-A and torque to 55 * lbf.in (6.2 Nm).

    4. Connect the electrical connector 4006VC-A to the EEC link harness receptacle and torque to 21 * lbf.in (2.4 Nm).

    5. Assemble the datum clip position 5750 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    6. Connect the electrical connector 4027KS-A to the ACC actuator and torque to 32 * lbf.in (3.6 Nm).

    7. Assemble the datum clip position 5711 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    8. Assemble the datum clip position 5765 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    9. Assemble the datum clip position 5693 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    10. NOTE

      Clip position 5222 was initially assembled in TASK 72-00-40-420-004.

      Pre SBE 71-0145: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820, 5801, 5800 and 6067.

      SBE 71-0145 and Pre SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820 and 6067.

      SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 6126, 6120 and 6067.

      Pre SBE 79-0087: Assemble the clip position 5927.

      Pre SBE 79-0087: Install the clip Fire Detection (System A) And Core Services Harness (71-52-41, 01-240) on the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) and assemble clip position 5222.

      SBE 75-0034 : Clip position 5745 - make sure that the clip is aligned correctly with the lip on the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070) to give a minimum clearance of 0.25 in (6.35 mm) between the master BSBVA actuator electrical connectors and the EEC harness.

      Torque the nuts and the bolts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).

    26. SUBTASK 72-00-40-420-212-C00 Install the EEC Harness, the Voltage Divider Harness and the Fire Detection (System B) Harness (Pre SBN 71-0145, SBN 71-0145, SBE 71-0303, Pre SBE 72-0553, SBE 75-0034, Pre SBE 79-0087 and SBE 79-0087)

      SBN 71-0145: Nacelle - Powerplant - Core fire detector - rework

      SBE 71-0303: EEC Harness- Fan Harness Core- Addition of a voltage divider harness assembly

      SBE 75-0034: Air - Replace HPC VSV actuator bracket assembly

      SBE 79-0087: Oil - Scavenge oil tubes - Re route of number 4 bearing scavenge tube

    2. Install the EEC harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005), the voltage divider harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005) and the fire detection (System B) harness ELECT HARNESS-LIGHT DUTY-FIRE DETECTION SYSTEM B (71-52-42, 01-005).

    3. Attach the two electrical receptacles 4008VC and 4009VC (with the master keyways to the front) to the bifurcation panel with the eight bolts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-022) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-027) and the nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-020) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-025). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm). Connect the two electrical connectors 4008VC-A and 4009VC-A and torque to 55 * lbf.in (6.2 Nm).

    4. Connect the electrical connector 4006VC-A to the EEC link harness receptacle and torque to 21 * lbf.in (2.4 Nm).

    5. Assemble the datum clip position 5750 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    6. Connect the electrical connector 4027KS-A to the ACC actuator and torque to 32 * lbf.in (3.6 Nm).

    7. Assemble the datum clip position 5711 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    8. Assemble the datum clip position 5765 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    9. Assemble the datum clip position 5693 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    10. NOTE

      Clip position 5222 was initially assembled in TASK 72-00-40-420-004.

      NOTE

      Do not torque the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-310) at the clip position 5732.

      Pre SBE 71-0145: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820, 5801, 5800 and 6067.

      SBE 71-0145 and Pre SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820 and 6067.

      SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 6126, 6120 and 6067.

      Pre SBE 79-0087: Assemble the clip position 5927.

      Pre SBE 79-0087: Install the clip Fire Detection (System A) And Core Services Harness (71-52-41, 01-240) on the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) and assemble clip position 5222.

      SBE 75-0034 : Clip position 5745 - make sure that the clip is aligned correctly with the lip on the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070) to give a minimum clearance of 0.25 in (6.35 mm) between the master BSBVA actuator electrical connectors and the EEC harness.

      Install the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-313) on the harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005), the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-203) on the harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005). Assemble the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-203), the spacer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-314), the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-313) and the spacer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-315) at the clip position 5732. Temporarily install the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-310) at the clip position 5732. Lightly tighten the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-310).

      Torque the nuts and the bolts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).

    27. SUBTASK 70-00-40-213-212-D00 Install the EEC Harness and the Fire Detection (System B) Harness (Pre SBE 71-0109, Pre SBN 71-0145, SBN 71-0145, SBE 72-0553, SBE 75-0034, Pre SBE 79-0087 and SBE 79-0087)

      SBN 71-0145: Nacelle - Powerplant - Core fire detector - rework

      SBE 72-0553: Introduction of new trim balance probe and deletion of related powerplant voltage divider harness assembly

      SBE 75-0034: Air - Replace HPC VSV actuator bracket assembly

      SBE 79-0087: Oil - Scavenge oil tubes - Re route of number 4 bearing scavenge tube

    2. Install the EEC harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005) and the fire detection (System B) harness ELECT HARNESS-LIGHT DUTY-FIRE DETECTION SYSTEM B (71-52-42, 01-005).

    3. Attach the two electrical receptacles 4008VC and 4009VC (with the master keyways to the front) to the bifurcation panel with the eight bolts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43,01-022) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-027) and the nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-020) and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-025). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm). Connect the two electrical connectors 4008VC-A and 4009VC-A and torque to 55 * lbf.in (6.2 Nm).

    4. Connect the electrical connector 4006VC-A to the EEC link harness receptacle and torque to 21 * lbf.in (2.4 Nm).

    5. Assemble the datum clip position 5750 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    6. Connect the electrical connector 4027KS-A to the ACC actuator and torque to 32 * lbf.in (3.6 Nm).

    7. Assemble the datum clip position 5711 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    8. Assemble the datum clip position 5765 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    9. Assemble the datum clip position 5693 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    10. NOTE

      Clip position 5222 was initially assembled in TASK 72-00-40-420-004.

      Pre SBE 71-0145: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820, 5801, 5800 and 6067.

      SBE 71-0145 and Pre SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 5821, 5820 and 6067.

      SBE 79-0087: Assemble the clip positions that follow:

      5817, 5840, 5751, 5733, 5732, 5774, 5773, 5712, 5660, 5689, 5688, 5763, 5764, 5725, 5745, 6126, 6120 and 6067.

      Pre SBE 79-0087: Assemble the clip position 5927.

      Pre SBE 79-0087: Install the clip Fire Detection (System A) And Core Services Harness (71-52-41, 01-240) on the harness Fire Detection (System A) And Core Services Harness (71-52-41, 01-005) and assemble clip position 5222.

      SBE 75-0034 : Clip position 5745 - make sure that the clip is aligned correctly with the lip on the bracket AIR-HP COMPRESSOR VARIABLE STATOR VANE ACTUATOR (75-32-41, 01-070) to give a minimum clearance of 0.25 in (6.35 mm) between the master BSBVA actuator electrical connectors and the EEC harness.

      Torque the nuts and the bolts at the clip positions to 36 to 45 lbf.in (4 to 5 Nm).

    28. SUBTASK 72-00-40-420-213-A00 Connect the EEC Harness (71-52-43,01-005) to the Fan Speed Terminal Block (Pre SBE 71-0303 and Pre SBE 72-0023)

    1. Refer to Figure.

    2. Connect the two N1 sensor leads (4000VS-5 and 4000VS-6) to terminals No. 5 and No. 6. Install the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 02-500). Torque the nuts to 20 to 26 * lbf.in (2.26 to 2.94 Nm).

    3. Connect the two N1 sensor leads (4000VS-1 and 4000VS-2) to terminals No. 1 and No. 2. Install the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 02-505). Torque the nuts to 20 to 26 lbf.in (2.26 to 2.94 Nm).

    4. Connect the two trim balance sensor leads (4000VS-7 and 4000VS-8) to terminals No. 7 and No. 8. Install the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 02-510). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm).

    29. SUBTASK 72-00-40-420-213-B00 Connect the EEC Harness (71-52-43,01-005) to the Fan Speed Terminal Block (Pre SBE 71-0303 and SBE 72-0023)

      SBE 72-0023: Addition of washers for connection of the terminal block and the EEC harness-core

    1. Refer to Figure.

    2. Connect the two N1 sensor leads (4000VS-5 and 4000VS-6) to terminals No. 5 and No. 6. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-006). Torque the nuts to 20 to 22 lbf.in (2.26 to 2.48 Nm).

    3. Connect the two N1 sensor leads (4000VS-1 and 4000VS-2) to terminals No. 1 and No. 2. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-006). Torque the nuts to 20 to 22 lbf.in (2.26 to 2.48 Nm).

    4. Connect the two trim balance sensor leads (4000VS-7 and 4000VS-8) to terminals No.7 and No.8. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-009). Torque the nuts to 10 to 11.5 lbf.in (1.13 to 1.30 Nm).

    30. SUBTASK 72-00-40-420-213-C00 Connect the EEC Harness (71-52-43,01-005) and the Voltage Divider Harness (71-52-43,06-005) to the Fan Speed Terminal Block (SBE 71-0303 and Pre SBE 72-0553)

      SBE 71-0303: EEC Harness - Fan Harness Core - Addition of a voltage divider harness assembly

    1. Refer to Figure and Figure.

    2. Connect the two N1 sensor leads (4000VS-5 and 4000VS-6) to terminals No.5 and No.6. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43,01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE(71-52-43,01-006). Torque the nuts to 20 to 22 lbfin (2.26 to 2.48 Nm).

    3. Connect the two N1 sensor leads (4000VS-1 and 4000VS-2) to terminals No. 1 and No. 2. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-006). Torque the nuts to 20 to 22 lbf.in (2.26 to 2.48 Nm).

    4. Connect the terminal lug B1 of the voltage divider harness assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005) and the trim balance sensor lead (4000VS-7) to terminal No. 7. Connect the terminal lug A1 of the voltage divider harness assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005) to terminal No. 8. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE(71-52-43,01-009). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm).

    5. Install the bolt assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-300) into the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-311) at the clip position 6150. Connect the grounding terminal lug E of the voltage divider harness assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005) and the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-311) to the bracket ENGINE-LP COMP/INTERMEDIATE CASE MODULE (72-32-00, 02-232). Install the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-308) and the nut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-314). Torque the nut to 40 lbf.in (4.5 Nm).

    6. Attach the terminal lug D of the voltage divider harness assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005) and the trim balance sensor lead (4000VS-8) to the bolt assembly ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-300). Install the nut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-320). Torque the nut to 10 to 14 lbf.in (1.13 to 1.58 Nm).

    7. Temporarily remove the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-310) at the clip position 5732. Assemble the grounding terminal lug C of voltage divider harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-005), the spacer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-314), the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 06-203), the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-313) and the spacer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-315) at the clip position 5732. Re-install the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-310). Torque the bolt to 40 lbf.in (4.5 Nm).

    31. SUBTASK 72-00-40-420-213-D00 Connect the EEC Harness (71-52-43,01-005) to the Fan Speed Terminal Block (SBE 72-0553)

      SBE 72-0553: Introduction of new trim balance probe and deletion of related powerplant voltage divider harness assembly

    1. Refer to Figure.

    2. Connect the two N1 sensor leads (4000VS-5 and 4000VS-6) to terminals No. 5 and No. 6. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43,01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-006). Torque the nuts to 20 to 22 lbf.in (2.26 to 2.48 Nm).

    3. Connect the two N1 sensor leads (4000VS-1 and 4000VS-2) to terminals No. 1 and No. 2. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-006). Torque the nuts to 20 to 22 lbf.in (2.26 to 2.48 Nm).

    4. Connect the two trim balance sensor leads (4000VS-7 and 4000VS-8) to terminals No. 7 and No. 8. Install the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-007) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-009). Torque the nuts to 10 to 14 lbf.in (1.13 to 1.58 Nm).

    32. SUBTASK 72-00-40-420-214 Connect the EEC Harness (01-005) to the T2.5 Thermocouple Terminal Block (4026KS-A)

    1. Refer to Figure.

    2. Connect the T2.5 thermocouple leads to the terminal block and install the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-015 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-017). Torque the top nut (01-015) to 8 to 12 * lbf.in (0.90 to 1.36 Nm.) and the lower nut (01-017) to 10 to 15 * lbf.in (1.13 to 1.69 Nm). Refer to the view at A.

    3. Remove the bolt ENGINE-INTERMEDIATE STRUCTURE (72-32-03, 01-510) from the bracket ENGINE-INTERMEDIATE STRUCTURE (72-32-03, 01-495) and attach the earth lead to the bracket with the bolt. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

    33. SUBTASK 72-00-40-420-215-A00 Install the Harness Clips and the Raceway (71-52-43,05-100) (Pre SBE 72-0132)

    1. Refer to Figure, Figure, Figure, and Figure.

    2. Assemble the datum clip position 5690 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      3. Install the raceway ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-100) at clip position 5744.

      1. Put the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-361) on the EEC harness adjacent to the lug on the tube 39. Attach the raceway and the harness to the lug on the tube 39 with the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-358), the washer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-359) and the nut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-365). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    4. Assemble the clip positions 5740, 5741 and 5743 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    34. SUBTASK 72-00-40-420-215-B00 Install the Harness Clips and the Raceway (71-52-43, 05-100) (SBE 72-0132)

      SBE 72-0132: LP compressor - Removal of stage 6 buffer air system

    1. Refer to Figure, Figure, Figure and Figure.

    2. Assemble the datum clip position 5690 and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      3. Install the raceway ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-100) at clip position 5744.

      1. Attach the raceway ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-100) to raceway BRACKETS & RACEWAYS-HARNESS SUPPORT-CORE (71-52-50, 04-100) with the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-358), the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-359) and the nut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-365). Torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    4. Assemble the clip positions 5740, 5741 and 5743 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm).

    35. SUBTASK 72-00-40-420-216-A00 Connect the EEC Harness Electrical Connectors to the VSV Actuator (Pre SBE 71-0063 and Pre SBE 71-0111)

    1. Refer to Figure.

    2. Connect the two electrical connectors 4022KS-B and 4022KS-C to the VSV actuator and torque to 8 * lbf.in (0.9 Nm).

    3. Connect the two electrical connectors 4022KS-A and 4022KS-D to the VSV actuator and torque to 12 * lbf.in (1.4 Nm).

    36. SUBTASK 72-00-40-420-216-B00 Connect the EEC Harness Electrical Connectors to the VSV Actuator,.nd (SBE 71-0063 and Pre SBE 71-0111)

      SBE 71-0063: EEC harness - Fan and EEC harness-core - Introduction of additional support for electrical connectors

    1. Refer to Figure and Figure.

    2. Connect the two electrical connectors 4022KS-B and 4022KS-C to the VSV actuator and torque to 8 * lbf.in (0.9 Nm).

      3. Assemble the clip position 5798.

      1. Install the two clips ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-488 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-489) on the backshells of the two connectors 4022KS-B and 4022KS-C.

      2. Attach the two clips together with the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-486), the two washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-487) and the nut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-493).

      3. Make sure the clips are in the correct position then torque the nut to 36 to 45 lbf.in (4 to 5 Nm).

    4. Connect the two electrical connectors 4022KS-A and 4022KS-D to the VSV actuator and torque to 12 * lbf.in (1.4 Nm).

      5. Assemble the clip positions 6060 and 6061.

      1. Install the two clips ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-505 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-513) on the backshells of the two connectors 4022KS-A and 4022KS-D.

      2. Put the bracket ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 05-940) in position. Attach the two clips to the bracket with the two bolts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-502 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-510), the four washers ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-503 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-511) and the two nuts ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-509 and ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE 01-517).

      3. Make sure the bracket and the two clips are in the correct position then torque the two nuts to 36 to 45 lbf.in (4 to 5 Nm).

      4. Safety the bracket to one of the connector backshells with CoMat 02-146 LOCKWIRE. Use the wire locking hole of the bracket and a wire locking hole in one of the backshell relief clamps.

    37. SUBTASK 72-00-40-420-216-C00 Connect the EEC Harness Electrical Connectors to the VSV Actuator (SBE 71-0111)

      SBE 71-0111: EEC harness fan/core - Deletion of clipping at VSVA and PMA harness connectors and introduction of wire locking to secure connectors.

    1. Refer to Figure.

    2. Connect the two electrical connectors 4022KS-B and 4022KS-C to the VSV actuator and torque to 8 * lbf.in (0.9 Nm).

    3. Safety the two connectors to each other with CoMat 02-126 LOCKWIRE.

    4. Connect the two electrical connectors 4022KS-A and 4022KS-D to the VSV actuator and torque to 12 * lbf.in (1.4 Nm).

    5. Safety the two connectors to each other with CoMat 02-126 LOCKWIRE.

    38. SUBTASK 72-00-40-420-217 Install the Ignition Supply Harness (Pre SBE 73-0006 and SBE 73-0006)

      SBE 73-0006: Fuel and control - Incorporate revised EBU harness clipping requirements at CP 5671 and CP 1097

    2. Install the ignition supply harness ELECT HARNESS-LIGHT DUTY-IGNITION SUPPLY HARNESS (71-51-44, 01-005).

    3. Assemble the datum clip positions 5675, 5557, 5679, 5780 and 5671 and torque the two bolts and the nut to 36 to 45 lbf.in (4 to 5 Nm).

    4. Assemble the clip positions that follow:

      Pre SBE 79-0087: 5696, 5595, 5695, 5772, 5714, 5713, 5694, 5692, 5691, 5678, 5779 and 5654.

      SBE 79-0087: 5696, 5595, 5695, 5772, 5714, 5713, 5694, 5692, 5691, 6110, 6114 and 6123.

      Torque the bolts and nuts to 36 to 45 lbf.in (4 to 5 Nm).

    39. SUBTASK 72-00-40-220-140-A00 Check the Clearances at Clip Positions 5696 and 5643 in the Area of the HPC Stage 7 Bleed Valve Duct and Tube (Pre SBE 72-0080)

    1. Refer to Figure.

    2. Check the clearance between the harness clip at the clip position 5696 and the HPC stage 7 bleed valve duct. An insufficient clearance is less than 0.100 in. (2.54 mm) or if the clip or harness is chafed.

    3. Check the clearance between the tube support bracket and tube 51 AIR-HP COMPRESSOR BLEED CONTROL TUBES (75-32-49, 13-500) at the clip position 5696 and 5643. An insufficient clearance is less than 0.100 in. (2.54 mm) or if the tube or bracket is chafed.

    4. If there is insufficient clearance in step B. or C. refer to SBE 72-0080.

    40. SUBTASK 72-00-40-220-140-B00 Check the Clearances at Clip Positions 5696 and 5643 in the Area of the HPC Stage 7 Bleed Valve Duct and Tube (SBE/SBN not-parse : 72-0080)

      SBE 72-0080: Replace a bracket at flange FJ

    1. Refer to Figure.

    2. Check the clearances.

    3. No action is necessary if the clearances agree with the clearances given in Fig.72-00-4-990-140-034.

    41. SUBTASK 72-00-40-420-249 Route and Attach the Right Hand Side and Left Hand Side EEC Harness Looms Together at the Bifurcation Panel (SBE 71-0109)

      SBE 71-0109: Provide improved routing and clipping of the EEC and ignition harness and raceway

    1. Refer to Figure.

      2. Attach the right hand side and left hand side EEC harness looms together at the bifurcation panel electrical connectors 4008VC-A and 4009VC-A.

      1. CAUTION

        YOU MUST ROUTE THE EEC HARNESS AND THE IGNITION SUPPLY HARNESS NEXT TO EACH OTHER TO THE ELECTRICAL CONNECTOR 4009VC-A. FOLLOW THE ROUTING PROCEDURE TO KEEP THE RIGHT SIDE EEC HARNESS FROM TOUCHING THE RIGHT SIDE C DUCT AND ADJACENT TUBE INSTALLATIONS.

        NOTE

        The EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-005) and the ignition supply harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-005) are installed in TASK 72-00-32-420-004-A00 (INSTALLATION-004, CONFIG-001).

        Make sure the installation of EEC harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-005) and the Ignition supply harness POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 01-005) is complete, this includes the installation of all the clip positions and connection of the all the electrical connectors. Make sure the harness routing is correct as follows :

      2. Make sure the left hand side harness is put in position forward of the right hand side harness (when viewed from the rear of the engine).

      3. Make sure that the right hand side ignition harness is routed with the right hand side EEC harness. Put the ignition harness on the forward side of the EEC harness through to the connector 4009VC-A. Both harnesses must go through clip position 1089.

      4. Make sure that the ignition harness goes through the gap below the right hand side and left hand side EEC harness looms (the harness looms which go to 4008VC-A and 4009VC-A). The ignition harness must be routed in a rearwards direction through clip position 0568.

      5. Attach the EEC harness looms together with lacing tape POWER PLANT-ELECTRICAL HARNESS-EEC HARNESS-FAN (71-51-41, 03-970) at the lowest point where the two looms meet (at the bottom dead center position).

      6. Tie the lacing and make secure, refer to the SPM TASK 70-43-02-400-501.

    42. SUBTASK 72-00-40-420-105-A00 Install the Fuel Drain Tubes (Pre SBE 75-0016)

      1. Install the tube 45 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-500). Refer to Figure.

      1. Connect the tube 45 to the ACC actuator and to the tube 216 at the bifurcation panel. Refer to Figure. Figure. Figure and Figure.

      2. Assemble the clip positions 5832 and 5833 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Assemble the clip position 5834 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Figure.

      4. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      2. Install the tube 47 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-500). Refer to Figure.

      1. Connect the tube 47 to the VSV actuator and to the tube 45.

      2. Assemble the clip position 5835 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      3. Install the tube 36 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-100). Refer to Figure.

      1. Connect the tube 36 to the tube 47.

      2. Assemble the clip position 5742 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      4. Install the tube 35 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-100). Refer to Figure.

      1. Connect the tube 35 to the tube 45.

      2. Assemble the clip position 5831 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

    43. SUBTASK 72-00-40-420-105-B00 Install the Fuel Drain Tubes (SBE 75-0016 and Pre SBE 79-0087)

      SBE 75-0016: Air - HPC bleed air tubes - Revised core engine tubes to improve clearance with harness bifurcation area - RH side

      1. Install the tube 45 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-500). Refer to Figure.

      1. Connect the tube 45 to the ACC actuator and to the tube 216 at the bifurcation panel. Refer to Figure. Figure. Figure and Figure.

      2. Assemble the clip positions 5832 and 5833 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Assemble the clip position 5640 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Figure.nd Figure.

      4. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      2. Install the tube 47 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-500). Refer to Figure.

      1. Connect the tube 47 to the VSV actuator and to the tube 45.

      2. Assemble the clip position 5835 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      3. Install the tube 36 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-100). Refer to Figure.

      1. Connect the tube 36 to the tube 47.

      2. Assemble the clip position 5742 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      4. Install the tube 35 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-100). Refer to Figure.

      1. Connect the tube 35 to the tube 45.

      2. Assemble the clip position 5831 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

    44. SUBTASK 72-00-40-420-105-C00 Install the Fuel Drain Tubes (SBE 79-0087)

      SBE 79-0087: Oil - Revised routing of EBU systems to allow re-routing of the oil scavenge tubes

      1. Install the tube 45 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-500). Refer to Figure.

      1. Connect the tube 45 to the ACC actuator and to the tube 216 at the bifurcation panel. Refer to Figure. Figure. Figure and Figure.

      2. Assemble the clip positions 5832, 5670, 6095 and 6109 and torque the nuts to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Assemble the clip position 5640 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Figure and Figure.

      4. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      2. Install the tube 47 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-500). Refer to Figure.

      1. Connect the tube 47 to the VSV actuator and to the tube 45.

      2. Assemble the clip position 6111 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connectors to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      3. Install the tube 36 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 01-100). Refer to Figure.

      1. Connect the tube 36 to the tube 47.

      2. Assemble the clip position 5742 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

      4. Install the tube 35 POWER PLANT-FUEL DRAIN TUBES-ENGINE (71-71-49, 02-100). Refer to Figure.

      1. Connect the tube 35 to the tube 45.

      2. Assemble the clip positions 5831 and 5714 and torque the nut to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure.

      3. Torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm) and safety with CoMat 02-126 LOCKWIRE.

    45. SUBTASK 72-00-40-420-106-A00 Install the LP Compressor Bleed Actuator Mount Brackets (Pre SBE 72-0051 and Pre SBE 72-0132)

      1. Install the slave bleed actuator mount bracket "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-200). Refer to Figure.

      1. Attach the guide "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-250) to the mount bracket with the bolt "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-265), the washer "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-267) and the clipnut "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-263). Align the holes in the guide with the holes in the mount bracket and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      2. Attach the mount bracket to the LP compressor/intermediate case rear frame with the four bolts "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-210). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

      2. Install the master bleed actuator mount bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-200). Refer to Figure.

      1. Attach the guide "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-250) to the mount bracket with the bolt "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-265), the washer "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-267) and the clipnut "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-263). Align the holes in the guide with the holes in the mount bracket and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      2. Attach the mount bracket to the LP compressor/intermediate case rear frame with the four bolts "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-210). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

    46. SUBTASK 72-00-40-420-106-B00 Install the LP Compressor Bleed Actuator Mount Brackets (SBE 72-0051 and SBE 72-0132)

      SBE 72-0051: LP compressor - Incorporate a fuel drain tube in the fan frame assembly.

      SBE 72-0132: LP compressor - Removal of stage 6 buffer air system.

      1. Install the slave bleed actuator mount bracket "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-200). Refer to Figure.

      1. Attach the guide "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-250) to the mount bracket with the bolt "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-265), the washer "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-267) and the clipnut "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-263). Align the holes in the guide with the holes in the mount bracket and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      2. Attach the mount bracket to the LP compressor/intermediate case rear frame with the four bolts "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-210). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm). Safety with CoMat 02-141 LOCKWIRE.

      2. Install the master bleed actuator mount bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-200) and the raceway bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-180). Refer to Figure.

      1. Attach the guide "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-250) to the mount bracket with the bolt "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-265), the washer "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-267) and the clipnut "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR(75-31-42, 01-263). Align the holes in the guide with the holes in the mount bracket and torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        2. Attach the mount bracket and the raceway bracket to the LP compressor/intermediate case rear frame.

        1. Attach the mount bracket to the LP compressor/intermediate case rear frame with two bolts "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-210). Install the bolts in the upper holes of the bracket.

        2. Attach the raceway bracket to the mount bracket and to the LP compressor/intermediate case rear frame with two bolts "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-210).

        3. Torque the four bolts to 85 to 105 lbf.in (10 to 12 Nm). Safety with CoMat 02-141 LOCKWIRE.

    47. SUBTASK 72-00-40-420-107 Install the LP Compressor Bleed Actuators (Pre SBE 75-0035 and SBE 75-0035)

      SBE 75-0035: Air - Revise the orientation of clipping point 5560

      1. Install the LP compressor slave bleed actuator "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-100). Refer to Figure.

      1. Attach the bleed actuator to the mount bracket with the three bolts "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-110), together with the bracket "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-090). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

      2. Attach the bleed valve actuating rod to the piston jack fork end with the bolt "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-125) and a new "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-115) keywasher1 off (Refer to SPM TASK 70-42-03-400-501). Torque the bolt to 50 to 60 * lbf.in (5.65 to 6.78 Nm).

        3. Assemble the clip position 5560.

        1. Install the clip ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-057) on the EEC harness adjacent to the bracket "AIR-LP COMPRESSOR BLEED,SLAVE ACTUATOR (75-31-43, 01-090).

        2. Pre SBE 75-0035 : Attach the clip to the bracket with the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-054), the washer ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-055) and the clipnut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-061). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

        3. SBE 75-0035 : Attach the clip to the bracket with the bolt ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-054) and the clipnut ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-061) refer to Figure. Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      4. Connect the drain tube (35) to the slave bleed actuator and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE. Refer to Figure.

        5. Connect the servo retract tube (33). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 15-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 33 to the bleed actuator and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

        6. Connect the servo extend tube (34). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 14-096) packing1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 34 to the bleed actuator and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

      2. Install the LP compressor master bleed actuator "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-100). Refer to Figure.

      1. Attach the bleed actuator to the mount bracket with the four bolts "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-110), together with the bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-080). Torque the bolts to 85 to 105 lbf.in (10 to 12 Nm).

      2. Attach the bleed valve actuating rod to the piston jack fork end with the bolt "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-125) and a new "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42,01-115) keywasher 1 off (Refer to the SPM TASK 70-42-03-400-501). Torque the bolt to 50 to 60 * lbf.in (5.65 to 6.78 Nm).

        3. Assemble the clip position 5533. Refer to Figure.

        1. Attach the raceway ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 05-900) to the bracket "AIR-LP COMPRESSOR BLEED,MASTER ACTUATOR (75-31-42, 01-080) with the bolt ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 05-901), the washer ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 05-902) and the clipnut ENGINE FUEL AND CONTROL-FUEL SYSTEM AIR TUBES (73-22-49, 05-908). Torque the bolt to 36 to 45 lbf.in (4 to 5 Nm).

      4. Connect the drain tube (36) to the bleed actuator and torque the tube connector to 159 to 177 lbf.in (18 to 20 Nm). Safety with CoMat 02-126 LOCKWIRE. Refer to Figure.

        5. Connect the servo return tube (41). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 16-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 41 to the bleed actuator and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

        6. Connect the servo supply tube (43). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 12-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 43 to the bleed actuator and torque the tube connector to 230 to 248 lbf.in (26 to 28 Nm). Safety with CoMat 02-126 LOCKWIRE.

        7. Connect the servo retract tube (33). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE(73-11-49, 15-096) packing1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 33 to the bleed actuator and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

        8. Connect the servo extend tube (34). Refer to Figure.

        1. Lightly lubricate a new ENGINE FUEL AND CONTROL-FUEL SYSTEM TUBES-ENGINE (73-11-49, 14-096) packing 1 off with CoMat 10-060 LIQUID PARAFFIN or CoMat 10-038 PETROLEUM JELLY. Install the packing on the bleed actuator. Connect the tube 34 to the bleed actuator and torque the tube connector to 204 to 221 lbf.in (23 to 25 Nm). Safety with CoMat 02-126 LOCKWIRE.

      9. Connect the electrical connector 4021KS-A and torque to 16 * lbf.in (1.8 Nm). Refer to Figure.

      10. Connect the electrical connector 4021KS-B and torque to 12 * lbf.in (1.4 Nm). Refer to Figure.

      11. NOTE

        These clip positions were assembled in Step.

        Torque the bolts and the nuts of the clip positions 5672, 5673, 5778, 5769 and 5775 to 36 to 45 lbf.in (4 to 5 Nm). Refer to Figure. Figure and Figure.

    48. SUBTASK 72-00-40-420-074 Install the Ignition Exciters (Pre SBE 74-0002, SBE 74-0002, Pre SBE 74-0003 and SBE 74-0003)

      SBE 74-0002: Engine - Ignition - Introduction of improved ignition lead, cooling shroud and the ignition cooling box.

      SBE 74-0003: Engine - Ignition - Introduction of a redimensioned ignition lead, cooling shroud and the deletion of ignition cooling box support bracket.

    1. Refer to Figure, Figure and Figure.

      2. Install the two high energy ignition exciters.

      1. Install the air seal washer IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-110) to the top ignition exciter.

      2. SBE 74-0002: Install the front ignition cooling box IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-100) and the rear ignition cooling box IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-102) to the top ignition exciter IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-120).

      3. SBE 74-0002 and Pre SBE 74-0003: Install the support brackets IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-095) to the cooling box assembly.

      4. SBE 74-0002: Install the locking washer nuts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-090) to the cooling box assembly.

      5. SBE 74-0002: Torque the 12 nuts to 20 to 26 lbf.in (2.26 to 2.94 Nm).

      6. Attach the top ignition exciter and cooling box assembly to the cross brackets (IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-200) and IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-270)) with the bolt IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-135), the nut IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-130), the two bolts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-150) and the two nuts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-145).

      7. WARNING

        WHEN YOU USE CoMat 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.

        Clean the bonding lead connector and the surface it touches on the exciter box and the remaining bolt IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-150) with CoMat 01-001 SOLVENT, DELETED. When the parts are dry install the bolt and the nut IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-145).

      8. Install the air seal washer IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-510) to the lower ignition exciter.

      9. SBE 74-0002: Install the front ignition cooling box IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-500) and the rear ignition cooling box IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-502) to the lower ignition exciter IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-520).

      10. SBE 74-0002 and Pre SBE 74-0003: Install the support brackets IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-495) to the cooling box assembly.

      11. SBE 74-0002: Install the locking washer nuts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-490) to the cooling box assembly.

      12. SBE 74-0002: Torque the 12 nuts to 20 to 26 lbf.in (2.26 to 2.94 Nm).

      13. Attach the lower ignition exciter and cooling box assembly to the cross brackets (IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-600) and IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-670)) with the bolt IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-535), the nut IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-530), the two bolts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-550) and the two nuts IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-545).

      14. WARNING

        WHEN YOU USE CoMat 01-002 SOLVENT, DELETED. INHIBITED AND STABILIZED TRICHLOROETHANE YOU MUST USE THE NECESSARY PROTECTIVE CLOTHING. DO NOT GET THE SOLVENT ON YOUR SKIN OR IN YOUR EYES. YOU MUST NOT SMOKE WHEN YOU USE THE SOLVENT AS THE VAPOR CHANGES AND BECOMES TOXIC.

        Clean the bonding lead connector and the surface it touches on the exciter box and the remaining bolt IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-550) with CoMat 01-001 SOLVENT, DELETED. When the parts are dry install the bolt and the nut IGNITION-EXCITER IGNITION UNITS (74-11-38, 01-545).

      15. Torque the six nuts to 36 to 45 lbf.in (4 to 5 Nm).

    3. Attach the top air inlet hose AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-100) in position with the two hose clamps AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-125) and AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-210). Tighten the hose clamps finger tight.

    4. Attach the lower air inlet hose AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-500) in position with the two hose clamps AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-525) and AIR COOLING-IGNITION COOLING LEADS (75-27-49, 01-610). Tighten the hose clamps finger tight.

    5. Connect the ignition lead IGNITION-IGNITION LEADS (74-21-43, 01-100) to the top ignition exciter and torque to 140 to 160 lbf.in (15.82 to 18.08 Nm).

    6. Pre SBE 74-0002 and Pre SBE 74-0003: Install the two cooling shrouds IGNITION-IGNITION LEADS (74-21-43, 01-030) and IGNITION-IGNITION LEADS (74-21-43 ,01-035) and the two clamps IGNITION-IGNITION LEADS (74-21-43, 01-015) and IGNITION-IGNITION LEADS (74-21-43, 01-020).

    7. SBE 74-0002 and SBE 74-0003: Install the cooling shroud IGNITION-IGNITION LEADS (74-21-43, 01-030) and the two clamps IGNITION-IGNITION LEADS (74-21-43, 01-015) and IGNITION-IGNITION LEADS (74-21-43, 01-020).

    8. Torque the two clamp screws to 20 to 25 lbf.in (2.26 to 2.82 Nm).

    9. Connect the ignition lead IGNITION-IGNITION LEADS (74-21-43, 02-100) to the bottom ignition exciter and torque to 140 to 160 lbf.in (15.82 to 18.08 Nm).

    10. Pre SBE 74-0002 and Pre SBE 74-0003: Install the two cooling shrouds IGNITION-IGNITION LEADS (74-21-43, 02-030) and IGNITION-IGNITION LEADS (74-21-43, 02-035) and the two clamps IGNITION-IGNITION LEADS (74-21-43, 02-015) and IGNITION-IGNITION LEADS (74-21-43, 02-020).

    11. SBE 74-0002 and SBE 74-0003: Install the cooling shroud IGNITION-IGNITION LEADS (74-21-43, 02-030) and the two clamps IGNITION-IGNITION LEADS (74-21-43, 02-015) and IGNITION-IGNITION LEADS (74-21-43, 02-020).

    12. Torque the two clamp screws to 20 to 25 lbf.in (2.26 to 2.82 Nm).

    13. Connect the electrical connector 4000JH1-A to the top ignition exciter and torque to 14 * lbf.in (1.6 Nm).

    14. Connect the electrical connector 4000JH2-A to the bottom ignition exciter and torque to 14 * lbf.in (1.6 Nm).

    49. SUBTASK 72-00-40-220-085 Measure the Harness Clearances and Examine the Harness Routing

    1. Refer to Figure.

      2. Measure the clearance between all the different harnesses and the engine parts.

      1. The general clearance must be a minimum of 0.250 in. (6.35 mm).

      2. A minimum clearance of 0.100 in. (2.54 mm) is necessary between the EEC harness ELECTRICAL HARNESS-LIGHT DUTY-EEC HARNESS-CORE (71-52-43, 01-005) and the tubes in the area shown. Refer to Figure.

      3. To check the clearance, push the harness with a light pressure of the thumb then release. The harness must spring back and give the minimum clearance. The harness must not move through the adjacent clips, refer to Step.

      4. The harness can touch the smooth parts of brackets if the harness is clipped to them. The harness must be held so there is no movement between the harness and the bracket.

    3. Adjust the harness (if necessary) to get the minimum clearance and torque the clip position nut or bolt to 36 to 45 lbf.in (4 to 5 Nm).

      4. Examine the harness routing.

      1. Make sure each wire bundle breakout curves smoothly from the primary harness and is in the direction of the component to which it connects. It must not go across the primary harness.

      2. If the primary harness, the wire bundle breakout or a different harness touch each other they must be attached to each other. Refer to Step. The bundles must not move in relation to each other.

    50. SUBTASK 72-00-40-420-132 Attach the Harness Together

    1. Attach the wire bundle breakout to the primary harness with CoMat 02-159 LACING TAPE so they do not move in relation to each other.

    2. Attach the parallel harnesses and those which go across each other together. If it is necessary, wrap CoMat 02-148 ADHESIVE TAPE (ELECTRICAL) around the harness (to prevent abrasion). Then attach them together with CoMat 02-159 LACING TAPE.

    51. SUBTASK 72-00-40-420-289 Seal the Electrical Harness Connections at the Bifurcation Panel (SBE 72-0193)

      SBE 72-0193: Core to fancase interface sealing of the bifurcation panel

    1. Refer to Figure.

    2. Clean the surface of the joint faces at the electrical connectors and fume and fireseal, Refer to Figure.

      Refer to the SPM TASK 70-11-26-300-503 for the procedure to locally swab clean.

    4. Locally swab clean the areas again, Refer to the SPM TASK 70-11-26-300-503.

    5. Use dry compressed air or CoMat 02-099 LINT-FREE CLOTH to dry the cleaned areas.

    6. Make sure that there are no remaining solvent cleaning fluids in the joints at the specified locations.

    7. NOTE

      For CoMat 08-013 COLD CURING SILICONE COMPOUND use CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT. For CoMat 08-074 SEALANT, RTV SILICONE use CoMat 08-032 PRIMER.

      Use a soft brush and apply a thin layer of primer to the cleaned areas.

      8. Dry the primer.

      2. For CoMat 08-032 PRIMER air dry for 60 to 90 minutes.

      9. Apply the sealant to seal the core receptacle to bifurcation panel joint.

      2. NOTE

        Apply the sealant in a thin layer, less than 0.120 in. (3.00 mm.) dia.

        Press the sealant into the clearances between the bifurcation panel and the connectors.

      10. Cure the sealant.

      1. NOTE

        1. The surface of the sealant can be touched after 12 hours.

        2. Do not apply a load during this time.

        For CoMat 08-013 COLD CURING SILICONE COMPOUND cold cure at 68 deg F (20 deg C) for 48 hours.

      2. NOTE

        1. The surface of the sealant can be touched after 1 or 2 hours.

        2. Do not apply a load during this time.

        For CoMat 08-074 SEALANT, RTV SILICONE cure at 77 deg F (35 deg C) for 24 hours.

    52. SUBTASK 72-00-40-210-057 Visually Inspect the Electrical Backshells and Cable Clamps

    1. Refer to Figure.

    2. Make sure that all the applicable connectors, backshells and cable clamps are secure.

    3. Make sure that all the applicable backshells and cable clamps are safetied with CoMat 02-126 LOCKWIRE. Refer to the SPM TASK 70-42-05-400-501.

    53. SUBTASK 72-00-40-210-058 Visually Inspect the EEC Harness (01-005) Electrical Backshells and Cable Clamps (SBE 70-0813)

      SBE 70-0813: Announcement of introduction of safety cable as a preferred method to lockwire.

    1. NOTE

      Use this procedure to safety the EEC harness backshells and cable clamps with safety cable.

      Refer to Figure.

    2. Make sure that all the EEC harness connectors, backshells and cable clamps are secure.

    3. Make sure that all the EEC harness backshells and cable clamps are safetied. Safety with CoMat 02-274 SAFETY CABLE KIT or with CoMat 02-275 SAFETY CABLE KIT. Refer to the SPM TASK 70-42-08-400-501.

    54. SUBTASK 72-00-40-420-162 Install the Forward Mount Assembly

    1. Install the forward mount as detailed in TASK 71-00-32-450-001 (INSTALLATION).

    55. Figure: Connect the Tubes at the Bifurcation Panel

    Sheet 1

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    Connect the Tubes at the Bifurcation Panel

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    Figure: Connect the Tubes at the Bifurcation Panel

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    Connect the Tubes at the Bifurcation Panel

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    Figure: Connect the Tubes at the Bifurcation Panel

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    Connect the Tubes at the Bifurcation Panel

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    Figure: Install the ACC Actuator

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    Install the ACC Actuator

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    Figure: Install the ACC Actuator

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    Install the ACC Actuator

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    Figure: Install the VSV Actuator

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    Install the VSV Actuator

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    Figure: Install the VSV Actuator

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    Install the VSV Actuator

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    Figure: Install the Raceways

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    Install the Raceways

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    Figure: Install the Raceways

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    Install the Raceways

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    Figure: Install the Raceways

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    Install the Raceways

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    Figure: SBN 70-0151 and Pre SBN 70-0151, SBN 72-0132 and Pre SBE 72-0132: Install the Raceways

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    SBN 70-0151 and Pre SBN 70-0151, SBN 72-0132 and Pre SBE 72-0132: Install the Raceways

    Sheet 4

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    Figure: Install the HP Servo Fuel Tubes

    Sheet 1

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    Install the HP Servo Fuel Tubes

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    Figure: Pre SBE 72-0132: Install the HP Servo Fuel Tubes

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    Pre SBE 72-0132: Install the HP Servo Fuel Tubes

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    Figure: SBE 72-0027, SBE 73-0115 and SBE 72-0132: Install the HP Servo Fuel Tubes

    Sheet 3

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    SBE 72-0027, SBE 73-0115 and SBE 72-0132: Install the HP Servo Fuel Tubes

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    Figure: Install the HP Servo Fuel Tubes

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    Install the HP Servo Fuel Tubes

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    Figure: Install the HP Servo Fuel Tubes

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    Install the HP Servo Fuel Tubes

    Sheet 5

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    Figure: SBE 72-0132, SBE 72-0027 and SBE 73-0103: Install the HP Servo Fuel Tubes

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    SBE 72-0132, SBE 72-0027 and SBE 73-0103: Install the HP Servo Fuel Tubes

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    Figure: Install the HP Servo Fuel Tubes

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    Install the HP Servo Fuel Tubes

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    Figure: Install the HP Servo Fuel Tubes

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    Install the HP Servo Fuel Tubes

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    Figure: Install the HP Servo Fuel Tubes

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    Install the HP Servo Fuel Tubes

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    Figure: Install the Fuel Distribution Feed Tube 62

    Install the Fuel Distribution Feed Tube 62

    Figure: Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

    Sheet 1

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    Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

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    Figure: Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

    Sheet 2

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    Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

    Sheet 2

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    Figure: Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

    Sheet 3

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    Install the HP Servo Fuel Tube 46 and the P2.5 Air Tubes 66 and 67

    Sheet 3

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    Figure: Install the No.1, 2 and 3 Bearing Oil Feed Tubes 57 and 58

    Install the No.1, 2 and 3 Bearing Oil Feed Tubes 57 and 58

    Figure: SBE 75-0011 and Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 1

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    SBE 75-0011 and Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 1

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    Figure: Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 2

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    Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 2

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    Figure: Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 3

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    Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 3

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    Figure: SBE 75-0011 and Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 4

    Legend
    SBE 75-0011 and Pre SBE 72-0132: Install the Front Bearing Compartment Buffer Air Tubes 30 and 39

    Sheet 4

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    Figure: Electrical Harness Installation Procedure

    Electrical Harness Installation Procedure

    Figure: Pre SBE 72-0132 and Pre SBE 79-0087: Install the Electrical Harnesses

    Sheet 1

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    Pre SBE 72-0132 and Pre SBE 79-0087: Install the Electrical Harnesses

    Sheet 1

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    Figure: Pre SBE 72-0132 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 2

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    Pre SBE 72-0132 and SBE 79-0087: Install the Electrical Harnesses

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    Figure: SBE 72-0132 and Pre SBE 79-0087: Install the Electrical Harnesses

    Sheet 3

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    SBE 72-0132 and Pre SBE 79-0087: Install the Electrical Harnesses

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    Figure: SBE 72-0132 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 4

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    SBE 72-0132 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 4

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    Figure: Pre SBE 72-0132, Pre SBE 79-0087, SBE 79-0087, Pre SBE 71-0303, SBE 71-0303, Pre SBE 72-0553 and SBE 72-0553: Install the Electrical Harnesses

    Sheet 5

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    Pre SBE 72-0132, Pre SBE 79-0087, SBE 79-0087, Pre SBE 71-0303, SBE 71-0303, Pre SBE 72-0553 and SBE 72-0553: Install the Electrical Harnesses

    Sheet 5

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    Figure: SBE 72-0132, Pre SBE 79-0087, SBE 79-0087, Pre SBE 71-0303, SBE 71-0303, Pre SBE 72-0553 and SBE 72-0553: Install the Electrical Harnesses

    Sheet 6

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    SBE 72-0132, Pre SBE 79-0087, SBE 79-0087, Pre SBE 71-0303, SBE 71-0303, Pre SBE 72-0553 and SBE 72-0553: Install the Electrical Harnesses

    Sheet 6

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    Figure: Install the Electrical Harnesses

    Sheet 7

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    Install the Electrical Harnesses

    Sheet 7

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    Figure: Pre SBE 71-0303, SBE 71-0303 and Pre SBE 72-0553: Install the Electrical Harnesses

    Sheet 8

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    Pre SBE 71-0303, SBE 71-0303 and Pre SBE 72-0553: Install the Electrical Harnesses

    Sheet 8

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    Figure: SBE 72-0553: Install the Electrical Harnesses

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    SBE 72-0553: Install the Electrical Harnesses

    Sheet 9

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    Figure: Pre SBE 70-0151, Pre SBE 71-0145, Pre SBN 71-0272, Pre SBE 79-0087 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 10

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    Pre SBE 70-0151, Pre SBE 71-0145, Pre SBN 71-0272, Pre SBE 79-0087 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 10

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    Figure: SBN 71-0272 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 11

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    SBN 71-0272 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 11

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    Figure: SBN 71-0272, Pre SBE 71-0295 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 12

    Legend
    SBN 71-0272, Pre SBE 71-0295 and SBE 79-0087: Install the Electrical Harnesses

    Sheet 12

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

    Sheet 15

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    Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Pre SBE 71-0303 and SBE 71-0303: Install the Electrical Harnesses

    Sheet 17

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    Pre SBE 71-0303 and SBE 71-0303: Install the Electrical Harnesses

    Sheet 17

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    Figure: SBE 72-0553: Install the Electrical Harnesses

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    SBE 72-0553: Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

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    Install the Electrical Harnesses

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    Figure: Install the Electrical Harnesses

    Sheet 25

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    Install the Electrical Harnesses

    Sheet 25

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    Figure: Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

    Sheet 26

    Legend
    Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

    Sheet 26

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    Figure: Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

    Sheet 27

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    Pre SBE 72-0132 and SBE 72-0132: Install the Electrical Harnesses

    Sheet 27

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    Figure: SBE 72-0132: Install the Electrical Harnesses

    Sheet 28

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    SBE 72-0132: Install the Electrical Harnesses

    Sheet 28

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    Figure: Pre SBE 70-0151 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 29

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    Pre SBE 70-0151 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 29

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    Figure: Pre SBE 79-0087 and Pre SBE 73-0006 and SBE 73-0006: Install the Electrical Harnesses

    Sheet 30

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    Pre SBE 79-0087 and Pre SBE 73-0006 and SBE 73-0006: Install the Electrical Harnesses

    Sheet 30

    Close

    Figure: Pre SBE 71-0065 and SBE 71-0065, Pre SBE 70-0151 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 31

    Legend
    Pre SBE 71-0065 and SBE 71-0065, Pre SBE 70-0151 and SBE 70-0151: Install the Electrical Harnesses

    Sheet 31

    Close

    Figure: Install the Electrical Harnesses

    Sheet 32

    Legend
    Install the Electrical Harnesses

    Sheet 32

    Close

    Figure: Install the Electrical Harnesses Pre SBE 72-0080: Check the Clearances at Clip Position 5696/5643

    Sheet 33

    Legend
    Install the Electrical Harnesses Pre SBE 72-0080: Check the Clearances at Clip Position 5696/5643

    Sheet 33

    Close

    Figure: Install the Electrical Harnesses SBE 72-0080: Check the Clearances at Clip Position 5696/5643

    Sheet 34

    Legend
    Install the Electrical Harnesses SBE 72-0080: Check the Clearances at Clip Position 5696/5643

    Sheet 34

    Close

    Figure: SBE 71-0063: Install the Electrical Harness

    Sheet 1

    Legend
    SBE 71-0063: Install the Electrical Harness

    Sheet 1

    Close

    Figure: SBE 71-0063 and Pre SBE 71-0111: Install the Electrical Harness

    Sheet 2

    Legend
    SBE 71-0063 and Pre SBE 71-0111: Install the Electrical Harness

    Sheet 2

    Close

    Figure: Pre SBE 75-0016, Pre SBE 79-0087 and SBE 75-0016: Install the Fuel Drain Tubes

    Sheet 1

    Legend
    Pre SBE 75-0016, Pre SBE 79-0087 and SBE 75-0016: Install the Fuel Drain Tubes

    Sheet 1

    Close

    Figure: Pre SBE 75-0016, SBE 75-0016 and SBE 79-0087: Install the Fuel Drain Tubes

    Sheet 2

    Legend
    Pre SBE 75-0016, SBE 75-0016 and SBE 79-0087: Install the Fuel Drain Tubes

    Sheet 2

    Close

    Figure: Install the Fuel Drain Tubes

    Sheet 3

    Legend
    Install the Fuel Drain Tubes

    Sheet 3

    Close

    Figure: Install the Fuel Drain Tubes

    Sheet 4

    Legend
    Install the Fuel Drain Tubes

    Sheet 4

    Close

    Figure: Install the Fuel Drain Tubes

    Sheet 5

    Legend
    Install the Fuel Drain Tubes

    Sheet 5

    Close

    Figure: Install the Fuel Drain Tubes

    Sheet 6

    Legend
    Install the Fuel Drain Tubes

    Sheet 6

    Close

    Figure: Install the LP Compressor Bleed Actuators

    Sheet 1

    Legend
    Install the LP Compressor Bleed Actuators

    Sheet 1

    Close

    Figure: Pre SBE 72-0132 and SBE 72-0132: Install the LP Compressor Bleed Actuators

    Sheet 2

    Legend
    Pre SBE 72-0132 and SBE 72-0132: Install the LP Compressor Bleed Actuators

    Sheet 2

    Close

    Figure: Install the LP Compressor Bleed Actuators

    Sheet 3

    Legend
    Install the LP Compressor Bleed Actuators

    Sheet 3

    Close

    Figure: Install the LP Compressor Bleed Actuators

    Sheet 4

    Legend
    Install the LP Compressor Bleed Actuators

    Sheet 4

    Close

    Figure: Pre SBE 74-0002 and Pre SBE 74-0003: Install the Ignition Exciters

    Sheet 1

    Legend
    Pre SBE 74-0002 and Pre SBE 74-0003: Install the Ignition Exciters

    Sheet 1

    Close

    Figure: Pre SBE 74-0002 and Pre SBE 74-0003: Install the Ignition Exciters

    Sheet 2

    Legend
    Pre SBE 74-0002 and Pre SBE 74-0003: Install the Ignition Exciters

    Sheet 2

    Close

    Figure: SBE 74-0002 and SBE 74-0003: Install the Ignition Exciters

    Sheet 3

    Legend
    SBE 74-0002 and SBE 74-0003: Install the Ignition Exciters

    Sheet 3

    Close

    Figure: Examine the Harness Routing

    Examine the Harness Routing

    Figure: SBE 71-0109 : Route and Attach the Right Hand Side and Left Hand Side EEC Harness Looms Together at the Bifurcation Panel

    SBE 71-0109 : Route and Attach the Right Hand Side and Left Hand Side EEC Harness Looms Together at the Bifurcation Panel

    Figure: Seal the Electrical Harness Connections at the Bifurcation Panel

    Seal the Electrical Harness Connections at the Bifurcation Panel

    Figure: Visually Inspect the Backshells and Cable Clamps

    Visually Inspect the Backshells and Cable Clamps

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
Manufacturer Code:01139
Enterprise Name:MOMENTIVE PERFORMANCE MATERIALS, INC
BU Name:MOMENTIVE PERFORMANCE MATERIALS, INC
Street:260 HUDSON RIVER RD
City:WATERFORD
State:NY
Zip Code:12188
Country:UNITED STATES OF AMERICA
Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:K3504
Enterprise Name:INDESTRUCTIBLE PAINT CO LTD
BU Name:NULL
Street:25 PENTOS DRIVE
City:SPARKHILL
Province:BIRMINGHAM
Zip Code:B11 3TA
Country:GREAT BRITAIN
Phone Number:44-121-7022485
Fax Number:44-121-7784338
Email:sales@indestructible.co.uk
Internet:www.indestructible.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Manufacturer Code:X111X
Supply Number:CoMat 01-001
Type:sp01
Supply Short Name:CoMat 01-001 SOLVENT, DELETED
Supply Name:CoMat 01-001 SOLVENT, DELETED
Specification Groups:
Doc NumberType
wiring harnesses. Where CoMat 01‐001 is specified to clean mechanical components, use one or more of the solvents that SPM TASK 70‐11‐26‐300‐503 specifies as applicable.DELETED. Where CoMat 01‐001 is specified to clean electrical contacts or wiring harnesses, use one or more of the solvents that SPM TASK 70‐11‐57‐110‐501 specifies to clean electrical contacts or
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:X111X
Supply Number:CoMat 01-002
Type:sp01
Supply Short Name:CoMat 01-002 SOLVENT, DELETED.
Supply Name:CoMat 01-002 SOLVENT, DELETED.
Specification Groups:
Doc NumberType
wiring harnesses. Where CoMat 01‐002 is specified to clean mechanical components, use one or more of the solvents that SPM TASK 70‐11‐26‐300‐503 specifies as applicable.DELETED. Where CoMat 01‐002 is specified to clean electrical contacts or wiring harnesses, use one or more of the solvents that SPM TASK 70‐11‐57‐110‐501 specifies to clean electrical contacts or
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:X222X
Supply Number:CoMat 02-099
Type:sp01
Supply Short Name:CoMat 02-099 LINT-FREE CLOTH
Supply Name:CoMat 02-099 LINT-FREE CLOTH
Specification Groups:
Doc NumberType
WHERE COMAT 02-099 IS SPECIFIED WITH NO SUFFIX, USE COMAT 02-099A OR COMAT 02-099B.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 02-119
Type:sp01
Supply Short Name:CoMat 02-119 LOCKWIRE
Supply Name:CoMat 02-119 LOCKWIRE
Specification Groups:
Doc NumberType
SAE AS9226 Part Number MS-9226-04 (0.032 IN DIA.)
Suppliers:
ManufacturerRemarks
LOCAL
51563
81343
V508V
Manufacturer Code:K6835
Supply Number:CoMat 02-126
Type:sp01
Supply Short Name:CoMat 02-126 LOCKWIRE
Supply Name:CoMat 02-126 LOCKWIRE
Specification Groups:
Doc NumberType
DTD 189A, 0.028 TO 0.032 IN DIA
Suppliers:
ManufacturerRemarks
K6835
KB362
LOCAL
U06C8
Manufacturer Code:LOCAL
Supply Number:CoMat 02-141
Type:sp01
Supply Short Name:CoMat 02-141 LOCKWIRE
Supply Name:CoMat 02-141 LOCKWIRE
Specification Groups:
Doc NumberType
AS3214-02 (0.8 mm)AMS 5689
Suppliers:
ManufacturerRemarks
LOCAL
81343
IE508
58401
Manufacturer Code:LOCAL
Supply Number:CoMat 02-146
Type:sp01
Supply Short Name:CoMat 02-146 LOCKWIRE
Supply Name:CoMat 02-146 LOCKWIRE
Specification Groups:
Doc NumberType
AIA/NAS NASM20995 Part Number MS20995C20 (0,5 MM)
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:LOCAL
Supply Number:CoMat 02-148
Type:sp01
Supply Short Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Supply Name:CoMat 02-148 ADHESIVE TAPE (ELECTRICAL)
Specification Groups:
Doc NumberType
OMAT: 296SCOTCH NO. 69 (WHITE)
Suppliers:
ManufacturerRemarks
LOCAL
76381
94960
K0993
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-159
Type:sp01
Supply Short Name:CoMat 02-159 LACING TAPE
Supply Name:CoMat 02-159 LACING TAPE
Specification Groups:
Doc NumberType
T085 OMAT: 274
Suppliers:
ManufacturerRemarks
LOCAL
IE218
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-274
Type:sp01
Supply Short Name:CoMat 02-274 SAFETY CABLE KIT
Supply Name:CoMat 02-274 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
SAE AS3510-0218K (DIA 0,032 IN LENGTH 18IN)
Suppliers:
ManufacturerRemarks
LOCAL
11851
U0419
70958
H7503
SA221
V384V
Manufacturer Code:X111X
Supply Number:CoMat 02-275
Type:sp01
Supply Short Name:CoMat 02-275 SAFETY CABLE KIT
Supply Name:CoMat 02-275 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
Deleted. Use CoMat 02-274.
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:LOCAL
Supply Number:CoMat 04-005
Type:sp01
Supply Short Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Supply Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Specification Groups:
Doc NumberType
OMAT: 4/47 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
JCR-026 (JAEC REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
DTD 900/4586 (RR REF, MOD UK REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
MSRR 9055 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
Suppliers:
ManufacturerRemarks
LOCAL
460Y4
CJ731
K3237
Manufacturer Code:0KHE3
Supply Number:CoMat 05-016
Type:sp01
Supply Short Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Supply Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Specification Groups:
Doc NumberType
GARNET PAPER, CAMI GRIT SIZE 80 GRADE 0 (ANSI B74.18)
Suppliers:
ManufacturerRemarks
0KHE3
1E1X8
LOCAL
C4347
K0993
K2F42
K6835
V571V
Manufacturer Code:0KHE3
Supply Number:CoMat 05-017
Type:sp01
Supply Short Name:CoMat 05-017 GARNET PAPER, 60 GRIT
Supply Name:CoMat 05-017 GARNET PAPER, 60 GRIT
Specification Groups:
Doc NumberType
GARNET PAPER, CAMI GRIT SIZE 60 GRADE 1/2 (ANSI B74.18)
Suppliers:
ManufacturerRemarks
0KHE3
1E1X8
C4347
LOCAL
K0993
K6835
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:X222X
Supply Number:CoMat 08-013
Type:sp01
Supply Short Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Supply Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Specification Groups:
Doc NumberType
If CoMat 08-013 is specified without an asterisk or a letter suffix, use one of the letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X222X
Supply Number:CoMat 08-014
Type:sp01
Supply Short Name:CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT
Supply Name:CoMat 08-014 PRIMER, SILICONE ADHESIVE/SEALANT
Specification Groups:
Doc NumberType
Use the applicable letter suffix material. Refer to SPM TASK 70-36-02-360-501.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X222X
Supply Number:CoMat 08-032
Type:sp01
Supply Short Name:CoMat 08-032 PRIMER
Supply Name:CoMat 08-032 PRIMER
Specification Groups:
Doc NumberType
DELETED. USE ONE OF THE COMAT 08-032 LETTER SUFFIX ALTERNATIVE MATERIALS.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 08-074
Type:sp01
Supply Short Name:CoMat 08-074 SEALANT, RTV SILICONE
Supply Name:CoMat 08-074 SEALANT, RTV SILICONE
Specification Groups:
Doc NumberType
N/A
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:K6835
Supply Number:CoMat 10-038
Type:sp01
Supply Short Name:CoMat 10-038 PETROLEUM JELLY
Supply Name:CoMat 10-038 PETROLEUM JELLY
Specification Groups:
Doc NumberType
SILKOLENE 775 CERTIFIED TO DEF STAN 91-38 GRADE PX-7 OR TO NATO S-743
Suppliers:
ManufacturerRemarks
K6835
U1757
Manufacturer Code:LOCAL
Supply Number:CoMat 10-060
Type:sp01
Supply Short Name:CoMat 10-060 LIQUID PARAFFIN
Supply Name:CoMat 10-060 LIQUID PARAFFIN
Specification Groups:
Doc NumberType
OMAT:CoMat 1020BP TECHNICAL WHITE OIL
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X
Manufacturer Code:LOCAL
Tool Number:0.937 in. (24.00 mm) crowsfoot spanner
Tool Name:0.937 in. (24.00 mm) crowsfoot spanner
Manufacturer Code:0AM53
Tool Number:IAE 1N20014
Tool Name:IAE 1N20014 Forward engine mount sling
Manufacturer Code:0AM53
Tool Number:IAE 1R18000
Tool Name:IAE 1R18000 Wrench
Manufacturer Code:0AM53
Tool Number:IAE 1R18001
Tool Name:IAE 1R18001 Wrench
Manufacturer Code:0AM53
Tool Number:IAE 1R18003
Tool Name:IAE 1R18003 Wrench
Manufacturer Code:0AM53
Tool Number:IAE 1R18254
Tool Name:IAE 1R18254 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R18282
Tool Name:IAE 1R18282 Rigging pin